NSN 6620-01-429-9115 · NIIN 014299115 · FSC 6620
NO DASHES 6620014299115
In Stock
COMPUTER,ENGINE
Engine Instruments
Application: F110-GE100 ENGINE F-16C/D ACFT
Technical characteristics
12 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| AGAV | END ITEM IDENTIFICATION | F110-GE100 ENGINE F-16C/D ACFT |
| AJAF | UNPACKAGED UNIT LENGTH | INCHES NOMINAL 10.00 |
| AJAG | UNPACKAGED UNIT WIDTH | INCHES NOMINAL 6.50 |
| AJAH | UNPACKAGED UNIT HEIGHT | INCHES NOMINAL 5.00 |
| AWZJ | POWER SOURCE | EXTERNAL OR SELF-CONTAINED |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| FEAT | SPECIAL FEATURES | AMBIENT OPERATING TEMPERATURE -65 TO +160 DEG F.;DOWNLOAD OPERATING POWER 20 WATTS;NORMAL OPERATING POWER 50 WATTS;THE EMSC IS AN AIRFRAME MOUNTED UNIT;BATTERY BACKUP |
| FTLD | FUNCTIONAL DESCRIPTION | RECEIVES DIGITAL ENGINE PERFORMANCE SIGNALS FROM THE ENGINE MONITORING SYSTEM PROCESSOR AND AIRCRAFT PARAMETERS FROM THE MUX;THESE SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMITS STORED IN THE EMSC;EXCEEDENCES AND FAULTS ARE TRANSMITTED TO REMOTE AIRCRAFT SYSTEMS;ALSO MONITORS THE DEC AND ITS OWN PERFORMANCES AND TRANSMITTS DATA TO THE PILOT DISPLAYS;DETECTS ENGINE CONTROL LOOP FAILURES AND COMPRESSOR STALLS |
| MATT | MATERIAL | CASE ALUMINUM ALLOY |
| RDAL | REFERENCE DATA AND LITERATURE | TO 5E1-2-12-1 |
| ZZZV | FSC APPLICATION DATA | ENGINE MONITORING SYSTEM COMPUTER (EMSC)SUPPGBATTERY NOT INCLUDED |
Supersedes
This item replaces cancelled NIINs 014178522 · 012135929 · 012521056 · 012474174 · 013107401. An older drawing citing one of those numbers resolves here.